# Service difficulty reports: N957AX, cancelled Sep 24, 2013

A list on [N957AX, cancelled Sep 24, 2013](https://openairdocs.org/deregistered/N957AX-2013-09-24.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR ABXA200811130264](https://openairdocs.org/sdr/ABXA200811130264.md): Battery Pack · discharged · Oct 24, 2008 · N957AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOP SWITCH LEFT ON. REPLACED EMERGENCY LIGHT BATTERY PACK AS PER DC9 MM 33-53-0.
- [SDR ABXA080243](https://openairdocs.org/sdr/ABXA080243.md): Tie Bolt · loose · Sep 24, 2008 · N957AX · Doug DC941 · Wheel/Ski/Float
  > LOOSE TIE BOLTS. WHEEL SCRAPPED. (K) TIE BOLT NUTS LOOSE REQUIRES REPAIR. INSPECTED, REPAIRED IAW ABX SPEC WORKSHEET BS421B DATED 12-21-07 AND THE ABX WHEEL AND TIRE MANUAL, REV 17.
- [SDR ABXA080142](https://openairdocs.org/sdr/ABXA080142.md): Floor Support · cracked · Apr 14, 2008 · N957AX · Doug DC941 · Fuselage Miscellaneous Structure
  > LATERAL FLOOR SUPPORT CRACKED AT FS 677, RIGHT BUTT LINE 30 & 34. REPLACED SUPPORT IAW DC9 SRM.
- [SDR ABXA070113](https://openairdocs.org/sdr/ABXA070113.md): Window Frame · cracked · Apr 5, 2007 · N957AX · Doug DC941 · Fuselage Main, Structure
  > WHILE COMPLYING WITH EA 53300036-003 COCKPIT WINDOW ENCLOSURE MOD PER AD 2002-21-09 DOUBLER WAS FOUND CRACKED. REPLACED PER EA 53300036-0034 THROUGH 017 AND WO 600265187, S/B DC9 53-290, DWG SR09530268.
- [SDR ABXA070110](https://openairdocs.org/sdr/ABXA070110.md): Window Frame · cracked · Apr 5, 2007 · N957AX · Doug DC941 · Fuselage Main, Structure
  > WHILE COMPLYING WITH EA 53300036-003, COCKPIT WINDOW ENCLOSURE MOD PER AD 2002-21-09, DOUBLER P/N: 991505-6 WAS FOUND CRACKED.5. REPLACED IAW EA 53300036-003 THROUGH 017 AND WO 600265187, S/B DC9 53-290 AND DWG SR09530268.
- [SDR ABXA070109](https://openairdocs.org/sdr/ABXA070109.md): Frame · cracked · Apr 5, 2007 · N957AX · Doug DC941 · Fuselage Main, Frame
  > WHILE COMPLYING WITH EA 53300036-003, COCKPIT WINDOW ENCLOSURE MOD PER AD 2002-21-09, DOUBLER P/N: 991505-5 WAS FOUND CRACKED.75. REPLACED IAW EA 53300036-003 THROUGH 017 AND WO 600265187, S/B DC9 53-290 AND DWG SR09530268.
- [SDR ABXA070108](https://openairdocs.org/sdr/ABXA070108.md): Frame · cracked · Apr 5, 2007 · N957AX · Doug DC941 · Fuselage Main, Frame
  > WHILE COMPLYING WITH EA 53300036-003, COCKPIT WINDOW ENCLOSURE MOD PER AD 2002-21-09, DOUBLER P/N: 991505-7 WAS FOUND CRACKED, 1.0" AND.875. REPLACED IAW EA 53300036-003 THROUGH 017 AND WO 600265187, S/B DC9 53-290 AND DWG SR09530268.
- [SDR ABXA070018](https://openairdocs.org/sdr/ABXA070018.md): Battery · discharged · Jan 25, 2007 · N957AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001.
- [SDR ABXA070013](https://openairdocs.org/sdr/ABXA070013.md): Smoke Detector · defective · Jan 19, 2007 · N957AX · Doug DC941 · Smoke Detection
  > AT FL320, LOWER CARGO FIRE LIGHT ILLUMINATED. LANDED AIRCRAFT. REPLACED SDU PER DC9 MM 26-15-00.
- [SDR ABXA070006](https://openairdocs.org/sdr/ABXA070006.md): Switch · loose · Jan 5, 2007 · N957AX · Doug DC941 · Exterior Lighting
  > NOSE LIGHT SWITCH SPARKED WHEN TURNED ON. RESECURED NOSE LANDING TAXI LIGHT, SWITCH NOW OPERATES NORMAL.
- [SDR ABXA060083](https://openairdocs.org/sdr/ABXA060083.md): Skin · cracked · Feb 6, 2006 · N957AX · Doug DC941 · Fuselage Main, Plate/Skin
  > RIGHT FS 147 BETWEEN LONGERON 18 - 19 RIGHT HAD SMALL CRACK IN SKIN. REPAIRED AREA IAW DC9 SRM 53-04.
- [SDR ABXA060082](https://openairdocs.org/sdr/ABXA060082.md): Skin · cracked · Feb 2, 2006 · N957AX · Doug DC941 · Fuselage Main, Plate/Skin
  > SKIN SPLICE CRACKED BETWEEN LONGERON 13 - 14 RIGHT, FS 1152 - 1163. STOP DRILLED CRACK. INSTALLED REPAIR IAW DC9 SRM 53-01, 51-30-2 AND 53-32-0.
- [SDR ABXA040271](https://openairdocs.org/sdr/ABXA040271.md): Skin · corroded · Jul 19, 2004 · N957AX · Doug DC941 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BULGED AND FASTENER POPPED AT FS 617, LONGERON 29 RIGHT. REPAIRED FUSELAGE SKIN AND INTERNAL DOUBLER AT STA 617 IAW DC-9 SRM 53-04.
- [SDR ABXA030144](https://openairdocs.org/sdr/ABXA030144.md): Stabilizer · vibration · May 15, 2003 · N957AX · Doug DC941 · Stabilizer Control System
  > SUSPECT FLIGHT CONTROL MALFUNCTION OF STABILIZER. DURING FLIGHT, THE AIRCRAFT EXHIBITED INCREASING TURBULANCE AND VIBRATION. THE AUTO PILOT WAS ENGAGED AND WORKING PROPERLY WITH NO NOTED PROBLEMS. FLIGHT LEVEL WAS AT 240, 330 KIAS. AS SOON AS AIRSPEED WAS REDU
- [SDR ABXA030073](https://openairdocs.org/sdr/ABXA030073.md): Intercostal · cracked · Jan 29, 2003 · N957AX · Doug DC941 · Fuselage Miscellaneous Structure
  > INTERCOSTAL WAS CRACKED TWO PLACES, FS 180, LBL 22. REPAIRED AREA IAW DC-9 SRM 51-10-3, 51-10-3B, AND REA D953-46196.
- [SDR ABXA030072](https://openairdocs.org/sdr/ABXA030072.md): Web · cracked · Jan 26, 2003 · N957AX · Doug DC941 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR UPPER AFT HINGE INTERCOSTAL WEB CRACKED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA030071](https://openairdocs.org/sdr/ABXA030071.md): Web · cracked · Jan 24, 2003 · N957AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED, LONGERON 18 LT, FS 1021 - 1041. REPLACED CUSP IAW DC-9 SRM 51-30-2.
- [SDR ABXA030070](https://openairdocs.org/sdr/ABXA030070.md): Fitting · cracked · Jan 23, 2003 · N957AX · Doug DC941 · Fuselage Main, Attach Fittings
  > FLOOR BEAM TO KEEL FITTING, STA. 775 WAS CRACKED. REPLACED FITTING, STA. 775, IAW DC-9 SRM 51-30-5 AND 51-30-1.
- [SDR ABXA030069](https://openairdocs.org/sdr/ABXA030069.md): Rib · cracked · Jan 23, 2003 · N957AX · Doug DC941 · Wing, Rib/Bulkhead
  > NR 2 SLAT TRACK CUT-OUT INBOARD LEADING EDGE RIB LOWER HORIZONTAL FLANGE HAD A 3.5 INCH CRACK. REPAIRED AREA IAW DC-9 REA D957-46167.
- [SDR ABXA010573](https://openairdocs.org/sdr/ABXA010573.md): Door · open · Nov 12, 2001 · N957AX · Doug DC941 · Landing Gear Door Retract Section
  > ON GEAR RETRACTION, RECEIVED SERIOUS VIBRATION AND A LOUD NOISE AS IF THE TIRE WAS STILL ROTATING. BUT WOULD NOT DISSIPATE AS IF TIRE SPIN STOPPED. ALL GEAR LIGHT INDICATIONS WERE NORMAL. GEAR RECYCLE. UPON ARRIVAL WHILE TAXIING TO BLOCKS, NOTICED THE RIGH
- [SDR ABXA010515](https://openairdocs.org/sdr/ABXA010515.md): Drive Link · binding · Sep 27, 2001 · N957AX · Doug DC941 · Landing Gear Door Retract Section
  > AFTER TAKEOFF WHEN THE LANDING GEAR WAS RAISED, A LOUD NOISE AND VIBRATIONS WERE NOTED FROM THE NOSE LANDING GEAR AREA. MAINTENANCE INSPECTED AND FOUND THE RIGHT NOSE LANDING GEAR OPEN ON THE TAXI IN. THE RIGHT FORWARD NOSE LANDING GEAR DOOR WAS FOUND TO BE
- [SDR ABXA010502](https://openairdocs.org/sdr/ABXA010502.md): Battery Pack · discharged · Sep 26, 2001 · N957AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW DC-9 MM 33-50-00.
- [SDR ABXA010382](https://openairdocs.org/sdr/ABXA010382.md): Control Box · faulty · Jul 10, 2001 · N957AX · Doug DC941 · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT WAS INTERMITTENTLY ON. RECYCLED GEAR, LIGHT REMAINED ON INTERMITTENTLY. OPERATED WITH RIGHT HYDRAULIC PUMP IN HIGH AND RESTRICTED AIRSPEED TO 300 KNOTS. REPLACED THE PROXIMITY CONTROL BOX AND THE MAIN GEAR UPLOC
- [SDR ABXA010354](https://openairdocs.org/sdr/ABXA010354.md): Fitting · cracked · Jun 12, 2001 · N957AX · Doug DC941 · Wing Structure
  > STRUCTURAL FITTING ON LEFT WING LEADING EDGE ON OUTBOARD SIDE OF #7 SLAT TRACK CRACKED BETWEEN TWO LOWER FASTENER HOLES. REPAIRED AREA IAW DC-9 REA D957-41317.
- [SDR ABXA010353](https://openairdocs.org/sdr/ABXA010353.md): Skin · chipped · Jun 8, 2001 · N957AX · Doug DC941 · Fuselage Structure (General)
  > FUSELAGE SKIN CRACKED OUT AT UPPER AFT CORNER OF MAIN ENTRY DOOR CUT-OUT. REPAIRED AREA IAW DC-9 REA D953-41305.
- [SDR ABXA9900752](https://openairdocs.org/sdr/ABXA9900752.md): Fitting · cracked · Oct 18, 1999 · N957AX · Doug DC941 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR LOWER FORWARD STOP FITTING CRACKED. REPLACED FITTING IAW DC9 MM 51-30-5.
- [SDR ABXA9900751](https://openairdocs.org/sdr/ABXA9900751.md): Skin · cracked · Oct 18, 1999 · N957AX · Doug DC941 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND CRACK IN SKIN AT LONGERON 14 RIGHT AND STATION 1072. REPAIRED IAW ABX REA D953-33715MR.
- [SDR ABXA9900822](https://openairdocs.org/sdr/ABXA9900822.md): Longeron · cracked · Oct 12, 1999 · N957AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 1041. REPLACED LONGERON SECTION IAW DC9 SRM 53-02-00.
- [SDR ABXA9900821](https://openairdocs.org/sdr/ABXA9900821.md): Shear Tie · cracked · Oct 12, 1999 · N957AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1021, LONGERON 15 AND 16 RIGHT. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2.
- [SDR ABXA9900744](https://openairdocs.org/sdr/ABXA9900744.md): Longeron · cracked · Oct 12, 1999 · N957AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 17 LEFT AT STATION 1041 CRACKED. REPLACED LONGERON SECTION IAW DC9 SRM 53-02.
- [SDR ABXA9800263](https://openairdocs.org/sdr/ABXA9800263.md): Blkhd Stiffener · cracked · Mar 26, 1998 · N957AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER 3RD UP FROM FLOOR, LEFT SIDE, CRACKED AT OUTBOARD END. REPAIRED STIFFENER IAW SERVICE REWORK DWG J060110.
- [SDR ABXA9800262](https://openairdocs.org/sdr/ABXA9800262.md): Blkhd Stiffener · cracked · Mar 26, 1998 · N957AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER 2ND UP FROM FLOOR, LEFT SIDE, CRACKED AT OUTBOARD END. REPAIRED STIFFENER IAW SERVICE REWORK DRAWING NR J060110..
- [SDR ABXA9800261](https://openairdocs.org/sdr/ABXA9800261.md): Bulkhead Tee · cracked · Mar 26, 1998 · N957AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD TEE-CAP SECTION NR 6 CRACKED. REPAIRED TEE-CAP IAW DWG SR09530056 AND ABX EA 53120037-006.
- [SDR ABXA9800260](https://openairdocs.org/sdr/ABXA9800260.md): Skin · corroded · Mar 26, 1998 · N957AX · Doug DC941 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, FOUND CORROSION ON LEFT HORIZONTAL STABILIZER UPPER SKIN FROM STATION XHS 32 - XHS 140. REPAIRED IAW ABX REA D955-2067.
- [SDR ABXA9800259](https://openairdocs.org/sdr/ABXA9800259.md): Fitting · cracked · Mar 26, 1998 · N957AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND KEEL AREA FITTING CRACKED AT STATION 737 AND RBL 8. REPLACED FITTING IAW DC9 SRM 51-30-1.
- [SDR ABXA9800258](https://openairdocs.org/sdr/ABXA9800258.md): Doubler · corroded · Mar 26, 1998 · N957AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL UPPER PRESSURE PANEL DOUBLER AT STATION 737 RBL 42 CORRODED. REPLACED DOUBLER IAW DC9 SRM 51-30-2.
- [SDR ABXA9700424](https://openairdocs.org/sdr/ABXA9700424.md): Skin · corroded · Jul 16, 1996 · N957AX · Doug DC941 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, FOUND CORROSION ON LEFT HORIZONTAL STABILIZER UPPER SKIN ABOVE THE REAR SPAR. REPAIRED IAW ABX REA D955-15636-MR.
- [SDR ABXA9700423](https://openairdocs.org/sdr/ABXA9700423.md): Bulkhead Dr Jamb · cracked · Jul 16, 1996 · N957AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND A RADIAL CRACK IN RIGHT UPPER CORNER OF APB VENTRAL DOOR JAMB. REPAIRED IAW ABX REA D953-15626-MR.
- [SDR ABXA9700470](https://openairdocs.org/sdr/ABXA9700470.md): Floor Support · cracked · Jul 12, 1996 · N957AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND FLOOR SUPPORT CRACKED AT STA 408. REPAIRED IAW ABX DRAWING K-05018.
- [SDR ABXA9700425](https://openairdocs.org/sdr/ABXA9700425.md): Support · cracked · Jul 12, 1996 · N957AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND FLOOR SUPPORT CRACKED AT STA 351. REPAIRED IAW ABX DRAWING K-05018.
- [SDR ABXA970078](https://openairdocs.org/sdr/ABXA970078.md): Bushing · worn · Jul 11, 1996 · N957AX · Doug DC941 · Landing Gear Door Retract Section
  > DURING C-CHECK AND COMPLIANCE WITH AD 91-22-07, FOUND RIGHT DOOR LINK TO DOUBLE ROD LINK HAS EXESSIVE PLAY. REPLACED BUSHING IAW DC-9 OHM 32-10-06.
- [SDR ABXA9700471](https://openairdocs.org/sdr/ABXA9700471.md): Bushing · worn · Jul 11, 1996 · N957AX · Doug DC941 · Landing Gear Door Retract Section
  > DURING C-CHECK AND COMPLIANCE WITH AD 91-22-07, FOUND LEFT FLYING DOOR TO DOUBLE ROD ATTACH LINK HAS EXCESSIVE PLAY. REPLACED BUSHING IAW DC-9 OHM 32-10-6.
- [SDR ABXA9600359](https://openairdocs.org/sdr/ABXA9600359.md): Retract Mech · malfunctioned · Mar 21, 1996 · N957AX · Doug DC941 · Landing Gear Retraction/Extension System
  > NOSE GEAR DID NOT COME OUT OF WELL, RECYCLED GEAR AND NOSE GEAR CAME DOWN. CHECKED NOSE GEAR LINKS AND MECHANISM, FOUND OK. PERFORMED RETRACTION CYCLE, CHECKED UP/DOWN FOR THREE TIMES. RETRACT OK, EXTENSION ON NOSE GEAR OK. THIS OPERATION DONE I/A/W DC9 MM
- [SDR ABXA9600265](https://openairdocs.org/sdr/ABXA9600265.md): Stringer Cap · corroded · Feb 2, 1996 · N957AX · Doug DC941 · Wing, Longeron/Stringer
  > DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND CORROSION IN STRINGER 20L AT T-CAP. REPAIRED IAW DC-9 SRM 51-10-3.
- [SDR ABXA9500680](https://openairdocs.org/sdr/ABXA9500680.md): Wire · loose · Aug 26, 1995 · N957AX · Doug DC941 · Landing Gear System Wiring
  > NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT WENT OUT. FOUND UPLOCK SENSOR GROUND WIRE LOOSE. SECURED GROUND WIRE, OPS CHECKED PROX SENSORS AND UNSAFE LIGHT IAW DC-9 SUPP MM 32-60-1. DURING GEAR SWING, ALL INDICATIONS OPS

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N957AX' AND deregistration_id = 'N957AX-2013-09-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N957AX-2013-09-24/reports

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